Paper
11 November 1999 Manufacture of a 2-m mirror with a glass membrane facesheet and active rigid support
James H. Burge, Brian Cuerden, Stephen M. Miller III, Robert C. Crawford, Helmuth H. Dorth, David G. Sandler, Richard W. Wortley
Author Affiliations +
Abstract
A 2-m diameter mirror is being manufactured as a demonstration for NASA's Next Generation Space Telescope (NGST). This mirror meets the challenging requirements of cryogenic operation and very low mass using an active control system. The mirror system consists of an aluminized glass membrane, 2 mm thick. This membrane is supported and controlled based on wavefront measurements with 169 remotely driven actuators. The system rigidity is provided by a lightweight carbon fiber composite structure. This entire mirror system, 2 meters across weighs less than 40 kg, and will demonstrate 20 nm surface quality in a cryogenic test facility at 35 K.
© (1999) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
James H. Burge, Brian Cuerden, Stephen M. Miller III, Robert C. Crawford, Helmuth H. Dorth, David G. Sandler, and Richard W. Wortley "Manufacture of a 2-m mirror with a glass membrane facesheet and active rigid support", Proc. SPIE 3782, Optical Manufacturing and Testing III, (11 November 1999); https://doi.org/10.1117/12.369178
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Cited by 2 scholarly publications.
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KEYWORDS
Actuators

Mirrors

Glasses

Cryogenics

Surface finishing

Polishing

Space telescopes

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